Understanding Watt & Newton: Questions for Physics Forum

Click For Summary

Discussion Overview

The discussion revolves around the concepts of watt and Newton, particularly in the context of a rocket in space. Participants explore the relationships between force, power, and energy consumption in various scenarios, including the effects of constant force and power over time.

Discussion Character

  • Exploratory
  • Technical explanation
  • Conceptual clarification
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant presents calculations showing that as a one Newton force is applied to a one kg rocket, the power appears to increase with time due to the acceleration of the rocket.
  • Another participant agrees that power increases with velocity when a fixed force is applied, but questions how velocity is determined in a vacuum where no external references exist.
  • Concerns are raised about the implications of using advanced propulsion methods, such as ion thrusters, and whether the principles discussed still apply in such cases.
  • A participant introduces a scenario involving kinetic energy and momentum conservation, questioning the outcomes of their calculations regarding the velocities of the rocket and ejected material.
  • Another participant confirms the correctness of the kinetic energy calculations presented, though no further details are provided.
  • A new participant seeks clarification on the relationship between watt and Newton, indicating a desire to understand the foundational concepts before addressing more complex questions.

Areas of Agreement / Disagreement

Participants express differing views on how power, force, and velocity interact in the context of a rocket in space. While some agree on certain principles, there is no consensus on the implications of these principles in specific scenarios, particularly regarding advanced propulsion systems and reference frames.

Contextual Notes

Participants' discussions include various assumptions about the conditions in space, such as the absence of gravity and external forces, which may affect their conclusions. The calculations presented rely on specific definitions and interpretations of energy, force, and power that may not be universally agreed upon.

Who May Find This Useful

This discussion may be of interest to those studying physics, particularly in the areas of mechanics, propulsion, and energy dynamics in space environments.

Stephanus
Messages
1,316
Reaction score
104
Dear Physics Forum,
I really don't understand the concept of watt and Newton.
I have two questions, perhaps someone can explain it to me.
=======================================================
Case 1:
If a one Newton force is applied to a one kg rocket in space with no or very little effect of gravity, for ...
A. 10 seconds, it will travel (1/2 x a x t^2 = 1/2 x 1 x10^2 = 50) 50 metres, it has consumed 50 joules, so its power is 5 watt.
B. 20 seconds, it will travel 200 metres, it consumes 200 joules, power is 10 watt.
C. 30 seconds, 450 metres, 450 joules, 15 watt
It seems that the power is increasing with each passing time(second). Its energy consume is not constant, but accelerating with each passing time.
Question1: Is that true?
======================================================
Case 2:
Before I ask, I would like to insert some equations here.
E = P.t (energy is power x time, second)
E = F.d (energy is force x distance, metre)
F = M.a (force is mass x accel)
d = 1/2 a.tt (dist is accel x time squared)
P.t = F.d
E = (F) x (d)
E = (M x a) x (1/2 a x tt)
E = 1/2 M x aa x tt
aa = 2E/M/tt
a = sqrt(2E/M)/t
F =
M x sqrt(2E/M)/t = sqrt(2EM)/t
d = 1/2 a.tt = sqrt(1/2 x E/M)/t x tt = sqrt(1/x2 x E/M) x t
Note:
F.d = sqrt(2EM)/t x sqrt(1/2 x E/M) x t = sqrt(2 x 1/2 x EE) x t / t = sqrt(EE) = E
F.d is of course (E)nergy
--------------------------------------------------------------------------------
A one kg rocket in space (no gravity) having a one watt power. Assuming it has a very, very efficient fuel, so the fuel mass loss is negligible.
A. After 2 seconds, its energy consume is 1 watt x 2 seconds = 2 Joule.
Its Force will be 1 Newton, its distance has to be 2 metres, 1 Newton x 2 metres = 2 joule
B. After 8 seconds, its energy consume is 8 joules
Its Force is 0.5 Newton x its distance is 16 metres = 8 joules
C. After 32 seconds , 32 joules
Force: 0.25 Newton, distance: 128 metres.
It seems with each passing time the force is diminishing.
Is that true?

Note: It will take 5.6 billion years to push it near the speed of light
11 billion years = twice the speed of light? But that's another question for relavity I think.
======================================================

Conclusion:
1. If the force is constant, does the power increase?
2. If the power is constant, does the force decrease?

Thanks for any answer.

Peace on earth

Steven
 
Physics news on Phys.org
Stephanus said:
If a one Newton force is applied to a one kg rocket in space with no or very little effect of gravity, for ...
A. 10 seconds, it will travel (1/2 x a x t^2 = 1/2 x 1 x10^2 = 50) 50 metres, it has consumed 50 joules, so its power is 5 watt.
B. 20 seconds, it will travel 200 metres, it consumes 200 joules, power is 10 watt.
C. 30 seconds, 450 metres, 450 joules, 15 watt
It seems that the power is increasing with each passing time(second). Its energy consume is not constant, but accelerating with each passing time.
Question1: Is that true?
Yes. The power produced from applying a fixed force increases with the velocity of its target.

A one kg rocket in space (no gravity) having a one watt power.
One watt power applied to what?

Rocket motors are normally rated based on their total power output -- power going to the craft plus power going to the exhaust stream. That power level turns out to be the same no matter how fast the rocket is moving.

The faster the craft is moving, the more power is going into accelerating the craft. And the less power is going into the exhaust stream. Go fast enough and the exhaust stream is actually less energetic than the unburned fuel (as viewed from the perspective of the ground that you are whizzing past).
 
  • Like
Likes   Reactions: Stephanus
Thank you for the answer Sir, (I guess you are male judging from you avatar)

Yes. The power produced from applying a fixed force increases with the velocity of its target.

"Power increases, applying a fixed force with the velocity"
I have a little "trouble" with the word "velocity" here.
- Supposed the target is in intergalactic void, with really no or miniscule gravity. How in the hell, (hell might be right if you're in Bootes void) that the rocket knows its velocity?. Supposed there is an astronout in that rocket and he when goes to sleep, the rocket accelerates for some hours and stops before he wakes up. After he wakes up, he would feel no acceleration at all, altough its speed might be hundreds of kms per hour. Does it require more power than before he slept, to thrust or add velocity to the rocket by 1 m/s?
-----------------------------------------------------------------------------------------------------------------

One watt power applied to what?

1. Rocket motors are normally rated based on their total power output...
2. The faster the craft is moving, the more power is going into accelerating the craft...
----------------
1. Supposed it does not use motor, but some very advanced ion thruster as in Startrek. That it ejects 1 molecule, or 1 polimer for that matter, near the speed of light to accel that 1 kg rocket by 1 m/s. Does the principle still apply?
2. The faster the craft...,
Perhaps you are referring air or ground friction or gravitation bound? Supposed the rocket is in intergalactic void where there's no friction or gravitation effect. Does it still require more power going into accelerationg the craft?

Again, thank you very much for you attention, sir.
 
Last edited:
Stephanus said:
"Power increases, applying a fixed force with the velocity"
I have a little "trouble" with the word "velocity" here.
- Supposed the target is in intergalactic void, with really no or miniscule gravity. How in the hell, (hell might be right if you're in Bootes void) that the rocket knows its velocity?.
Pick a reference frame, any reference frame. The principle applies regardless.

1. Supposed it does not use motor, but some very advanced ion thruster as in Startrek. That it ejects 1 molecule, or 1 polimer for that matter, near the speed of light to accel that 1 kg rocket by 1 m/s. Does the principle still apply?
Yes. Do the math. Take a 1.000001 kg object at rest and eject one milligram of exhaust at 1000 meters per second. Compute the total energy of the remaining 1 kg object and of the 1 milligram exhaust. Repeat the exercise but assume that the object starts with a velocity of one meter per second.

Compute the amount by which total energy increases in the first case.
Compute the amount by which total energy increases in the second case.
Compare the two.
 
Dear PF Forum,
Can I refresh my understanding of kinetic energy?
Supposed a rocket floating in space. With relative velocity 0 wrt to a planet. Let's say that the rocket is some distance away, so that the effect of that planet gravity is very small.
The rocket is 11 kg.
Then, the rocket propels its material 1 kg to the "west".
It only produces 220 joules for that process.
In momentum conservation, we'll have...
##m_1u_1 + m_2u_2 = m_1v_1 + m_2v_2##
Here:
m1: 10 kg
m2: 1 kg
n: The ratio m1/m2 = 10
Because u1 and u2 is zero, the rocket is at rest first wrt planet, so
##0 = m_1v_1 + m_2v_2##
The rocket produces 220 joules for the ejecting process, so...
##\frac{1}{2}m_1v_1^2 + \frac{1}{2}m_2v_2^2 = 220##
##m_1v_1 = -m_2v_2##
##m_2 = \frac{1}{n}m_1##
##v_2 = -nv_1##
combine those equations, we'll have
##\frac{1}{2}m_1v_1^2 + \frac{1}{2}nm_1v_1^2 = 220##
##\frac{1}{2}m_1v_1^2(1+n) = 220##
##v_1 = 2##
So, M1 will travel to the 'east' 2 m /s and m2 will travel to the 'west' 20 m/s is that so?

Thanks for any reply
 
  • Like
Likes   Reactions: Qwertywerty
Yes , I believe it's correct .
 
Dear PF Forum,
I have a question about rocket problem. That I asked in previous thread, but I didn't get enough feed back.
Actually I want to know the relation between watt and Newton/power and force. But before that I'd like to know about this answers first.
A rocket is floating in space.
The mass of the rocket: 1,000 kg.
The rocket spends energy for this action for 7,200,000 joules
Let's say n is 10
So the rocket eject 1/10th of it's mass backward to propel the rocket forward.
So ##M_{rocket} = 1000 kg##
##M_{body} = M_1; M_{ejecta} = M_2##

Based on momentum equation
##M_1 * V_1 = M_2 * V_2##
Based on kinetic energy equation
##0.5 M_1 * {V_1}^2 + 0.5 M_2 * {V_2}^2 = 7,200,000 joules##

So, trough a lengthy calculation I come up with this:
##M_1 = 900 kg##
##M_2 = 100 kg##, that is easy enough.
##V_1 = 40m/s##
##V_2 = 360m/s##

I calculate the energy consumed by each objects
##Ek_{body} = 0.5 * 900 kg * 40 * 40 = 720,000 joules##
##Ek_{ejecta} = 0.5 * 100 kg * 360 * 360 = 6,480,000 joules##

So the rocket consumes energy much smaller then its ejecta?I play around with n. Now I plug 100 into n
It means that the rocket throw 1/100th of its mass as the ejecta, to propel forward according to Newton third law:

##M_1 = 990kg##
##M_2 = 10kg##
##V_1 = 12.06m/s##
##V_2 = 1,193.98m/s##
##Ek_1 = 72,000 joules##
##Ek_2 = 7,128,000 joules##
That low?

n=1000
##Ek_1 = 7,200 joules##
##Ek_2 = 7,192,800 joules##

Is my calculation wrong? So a rocket really wastes its energy enormously?
 
I think your calculation might be right but your assumption for n is not realistic. Most real life rockets have n=1.11 to 1.25.

Also, all rockets that have achieved orbit are multiple stage rockets so there is an additional loss of mass there.
 
Which previous thread?

In terms of energy that goes to rocket and exhaust, rockets are horribly inefficient at low speeds, that is correct. There is no more efficient way in space, however. In an atmosphere, you can accelerate the air around the rocket, which is much more effective.

The ratio is better in a frame where the rocket has some initial speed. That shows that the energy ratio is not a very useful quantity. Rockets are all about velocity changes ("delta v").
 
  • #10
Stephanus said:
That I asked in previous thread, but I didn't get enough feed back.
Now you have one thread with plenty of feedback.

As was told to you each and every time you asked, yes, most of a rocket's energy goes into the exhaust at low speeds where they are very inefficient.

Thread closed. And don't reopen another one, the answer is still the same as the first three times and there is no need to say it again.
 
  • Like
Likes   Reactions: vanhees71

Similar threads

  • · Replies 138 ·
5
Replies
138
Views
9K
  • · Replies 1 ·
Replies
1
Views
1K
  • · Replies 17 ·
Replies
17
Views
3K
  • · Replies 7 ·
Replies
7
Views
3K
  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 17 ·
Replies
17
Views
3K
  • · Replies 29 ·
Replies
29
Views
4K
  • · Replies 12 ·
Replies
12
Views
2K
  • · Replies 9 ·
Replies
9
Views
2K
  • · Replies 27 ·
Replies
27
Views
2K